Field

Description

engine

Name

origin

Country of origin

designer

Name of company designed this engine

vehicle

Vehicle name where it is used

use

Location in the vehicle. Could be "Upper" for upper stage, "1st" for first stage, "2nd" for second stage & etc

propellant

Rocket propellant is a material used either directly by a rocket as the reaction mass that is ejected, typically with very high speed, from a rocket engine to produce thrust

specificImpulse

Specific impulse is a measure of how effectively a rocket uses propellant or jet engine uses fuel. Measured in seconds

thrust

Measured in newtons

mass

Mass in kilogram

thrustWeightRatio

Thrust-to-weight ratio is a dimensionless ratio of thrust to weight of a rocket, jet engine, propeller engine, or a vehicle propelled by such an engine that indicates the performance of the engine or vehicle.

chamberPressure

Pressure in rocker chamber. Measure in "bar"

oxidiserToFuelRatio